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CESSNA
MODEL
182S
SECTION
9.
SUPPLEMENTS
SUPPLEMENT
15
-
FAA APPROVED
SECTION
3
EMERGENCY PROCEDURES
The four step
procedure
listed under paragraph
A
should
be
among
the
basic airplane emergency procedures
that are
committed
to
memory.
lt is
important
that
the
pilot
be
proficient
in
accomplishing
all
four steps without reference to
this
manual.
1.
ln
case
of
Autopilot, Autopilot Trim,
or
Manual Electric
Trim
malfunction (accomplish ltems A and
B
simultaneously):
A. Airplane Control
Wheel
--
GRASP FIRMLY
and
regain
aircraft control.
B.
A/P
DISC/TRIM
INT
Switch
PRESS
and
HOLD
throughout recovery.
C. AIRCRAFT -- RE-TRIM Manually as Needed.
D.
AUTO
PILOT Circuit Breaker
--
PULL.
NOTE
The
AVIONICS MASTER Switch
may
be
used
as
an I
alternate means
of
removing
all
electric power from
the
autopilot
and
ms.
lf
necessary
perform
steps 1A
th
then turn
tre Áviot'llCS
I
MASTER
Sw
ating and pulling the
AUTO I
PILOT
Circu
the
AVIONICS
MASTER
I
Switch on as soon as
possible
to
restore power
to all
other
avionics
equipment.
Primary attitude, airspeed,
directional
compass, and altitude
instruments
will remain operational
at
alltimes.
¡[, wnnuno
DO
NOT
ATTEMPT
TO
RE.ENGAGE
THE
AUTOPILOT FOLLOWING
AN
AUTOPILOT,
AUTOTRIM,
OR
MANUAL ELECTRIC
TRIM
MALFUNCTION UNTIL
THE
CAUSE FOR
THE
MALFUNCTION
HAS BEEN CORRECTED.
Maximum Altitude losses
due
to autooilot malfunction:
CONFIGURATION
ALT.
LOSS
Cruise, Climb,
Descent
250
ft.
Maneuvering
100 ft.
Approach
50
ft.
Dec
31/99
s15-15
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